Xin Wang
Optimal Power Flow Based Architecture Design for Electrical Power System in More-Electric Aircraft
Wang, Xin; Atkin, Jason; Bozhko, Serhiy; Hill, Christopher Ian
Authors
JASON ATKIN jason.atkin@nottingham.ac.uk
Associate Professor
Professor SERHIY BOZHKO serhiy.bozhko@nottingham.ac.uk
Professor of Aircraft Electric Power Systems
Christopher Ian Hill
Abstract
When designing an electric power system (EPS) architecture for a more electric aircraft (MEA), the total weight of the system is treated as one of the most important criteria. For the weight saving purpose, this paper proposes an optimal power flow (OPF) based architecture design method to minimise the redundancy of the EPS of MEA, which includes reducing the generator overloading requirements for lighter generator design, and cutting down the excessive harness and number of contactors to lighten the wiring system. Based on the formulized mixed-integer linear programming (MILP) model, the addressed optimal architecture design (OAD) problem can be solved by optimising the power routing with minimum transmission losses in different flight stages simultaneously to minimise generator sizing and number of connections. The model contains both decision variables indicating the system architecture (e.g. cables existences and generator capacity) and the ones indicating the power flows with regards to the flight stages. In addition, the total transmission losses in the system are considered by formulizing the non-linear transmission losses of the DC/DC converters and cables losses in model constraints. By minimising the transmission losses, the generator overload capacity, as well as the cable needed for the connections, an optimised architecture with less redundancy and having optimal power routing in different flight stages can be realized, leading to lighter generator and wiring system for EPS.
Citation
Wang, X., Atkin, J., Bozhko, S., & Hill, C. I. (2019, October). Optimal Power Flow Based Architecture Design for Electrical Power System in More-Electric Aircraft. Presented at IEEE 45th Annual Conference of the Industrial Electronics Society (IECON'2019), Lisbon, Portugal
Presentation Conference Type | Conference Paper (published) |
---|---|
Conference Name | IEEE 45th Annual Conference of the Industrial Electronics Society (IECON'2019) |
Start Date | Oct 14, 2019 |
End Date | Oct 17, 2019 |
Acceptance Date | Apr 4, 2019 |
Online Publication Date | Oct 17, 2019 |
Publication Date | Oct 17, 2019 |
Deposit Date | Oct 24, 2019 |
Publicly Available Date | Oct 24, 2019 |
Book Title | Proceedings of the IEEE 45th Annual Conference of the Industrial Electronics Society (IECON'2019) |
Keywords | optimal architecture design; optimal power flow; transmission losses; wiring redundancy; electric power system; more electric aircraft |
Public URL | https://nottingham-repository.worktribe.com/output/2956746 |
Related Public URLs | https://iecon2019.org/ |
Additional Information | © 2019 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting/republishing this material for advertising or promotional purposes, creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works |
Contract Date | Oct 24, 2019 |
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